View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 43678U 18084H 23090.52704722 .00002569 00000-0 25201-3 0 9997
2 43678 98.0078 233.0044 0010713 61.4777 298.7521 14.93104227240678
Epoch (UTC): | 31 March 2023 12:38:56 |
Eccentricity: | 0.0010713 |
inclination: | 98.0078° |
perigee height: | 581 km |
apogee height: | 596 km |
right ascension of ascending node: | 233.0044° |
argument of perigee: | 61.4777° |
revolutions per day: | 14.93104227 |
mean anomaly at epoch: | 298.7521° |
orbit number at epoch: | 24067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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